CN103412311A - Pulse digitalized radar - Google Patents
Pulse digitalized radar Download PDFInfo
- Publication number
- CN103412311A CN103412311A CN2013102967081A CN201310296708A CN103412311A CN 103412311 A CN103412311 A CN 103412311A CN 2013102967081 A CN2013102967081 A CN 2013102967081A CN 201310296708 A CN201310296708 A CN 201310296708A CN 103412311 A CN103412311 A CN 103412311A
- Authority
- CN
- China
- Prior art keywords
- signal acquisition
- acquisition process
- radar
- process device
- signal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
- Y02A90/10—Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation
Landscapes
- Radar Systems Or Details Thereof (AREA)
Abstract
The invention relates to a pulse digitalized radar. The input end of a magnetron transmitter is connected with the output end of a signal acquisition processor; the output end of the magnetron transmitter is connected with an antenna through a transmit-receive switch; the transmit-receive switch is connected with a high frequency amplifier through a limiter; the high frequency amplifier is connected with a logarithmic demodulating receiver; the logarithmic demodulating receiver is connected with the input end of an AFC circuit through a frequency discriminator; the output end of the AFC circuit is connected with the high frequency amplifier; the output end of the logarithmic demodulating receiver is connected with the input end of the signal acquisition processor; the signal acquisition processor performs calculation so as to obtain signal basic information; and the output end of a servo module is connected with the signal acquisition processor. According to the pulse digitalized radar of the invention, signals received by the radar are subjected to distance accumulation and intensity correction, and then the signals are sent to and are displayed by an upper computer, and corresponding meteorological product data can be obtained through calculation. Compared with meteorological radars in similar types, the pulse digitalized radar is advantageous in compact structure, accurate measurement, convenient use and strong maintainability.
Description
Technical field
The present invention relates to a kind of radar system, refer to especially a kind of pulse digital radar.
Background technology
At present, for conventional digitized radar, can meet the needs of detection and the routine observation application in large zone, but be aimed at local small-scale synoptic process, can only carry out rough observation, if in mountain area, carry out the sexual intercourse detection, the scanning area of large radar is wider, unavoidably there is blind area to produce, if carry out synoptic process observation in the blind area of large radar, set up such digitized radar, be undoubtedly the cost costliness, and the radar service efficiency is low.
Summary of the invention
For above-mentioned deficiency, the purpose of this invention is to provide a kind of miniaturization, low cost, the high-precision interior pulse digital radar used of surveying among a small circle.
Technical scheme of the present invention is achieved in that a kind of pulse digital radar, comprises magnetron transmitter, signal acquisition process device, transmit-receive switch, antenna, limiter, radio-frequency amplifier, logarithmic detector receiver, AFC circuit, frequency discriminator, servo module; The input end of described magnetron transmitter is connected with the output terminal of signal acquisition process device, and the output terminal of described magnetron transmitter is connected with antenna by transmit-receive switch; Described transmit-receive switch is connected with radio-frequency amplifier by limiter, and described radio-frequency amplifier is connected with the logarithmic detector receiver; Described logarithmic detector receiver is connected with the input end of AFC circuit by frequency discriminator, and the output terminal of described AFC circuit is connected with radio-frequency amplifier; The output terminal of logarithmic detector receiver connects the input end of signal acquisition process device, and this signal acquisition process device calculates the signal essential information; The output terminal of described servo module is connected with the signal acquisition process device, and this servo module is input to antenna corner brace information and duty in the signal acquisition process device.
Further, described servo module comprises stepper motor, scrambler and transmission shaft, and described stepper motor and scrambler are positioned at the transmission shaft both sides.
Further, described signal acquisition process device is provided with A/D modular converter and D/A modular converter.
Further, described magnetron transmitter structure comprises magnetron and connected modulation module.
Further, on described signal acquisition process device, be connected with PC.
Compared with prior art, beneficial effect of the present invention is: after adopting said structure, the signal acquisition process device is controlled the triggering magnetron transmitter and is utilized trigger pip to carry out the control of signals collecting to the spatial emission pulse signal and when receiving signal, in order in data handling procedure, can more accurately calculate the strength information of radar return signal, by trigger pip, the skew of AFC circuit signal can be loaded on radio-frequency amplifier simultaneously, make the reception signal of weather radar keep with the frequency channel range, signal is stronger.Radar return signal accumulates by distance, and intensity is corrected, and finally sends into host computer and shows, calculates relative Meteorological Products data.It with of the same type be that weather radar is compared, compact conformation, measure accurately, easy to use, maintainability is strong.
In addition, small product size of the present invention is small and exquisite, flexible operation, but single-point arrange, also can arrange onboard and move, coordinate different meteorological software systems, carry out networking and process analysis procedure analysis afterwards.
The accompanying drawing explanation
In order to be illustrated more clearly in the embodiment of the present invention or technical scheme of the prior art, below will the accompanying drawing of required use in embodiment or description of the Prior Art be briefly described, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skills, under the prerequisite of not paying creative work, can also obtain according to these accompanying drawings other accompanying drawing.
Fig. 1 is structural representation of the present invention;
Fig. 2 is software principle figure of the present invention.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is clearly and completely described, obviously, described embodiment is only the present invention's part embodiment, rather than whole embodiment.Based on the embodiment in the present invention, those of ordinary skills, not making under the creative work prerequisite the every other embodiment obtained, belong to the scope of protection of the invention.
A kind of pulse digital radar as depicted in figs. 1 and 2, the input end of described magnetron transmitter 1 is connected with the output terminal of signal acquisition process device 10; The output terminal of magnetron transmitter 1 is connected with antenna 3 by transmit-receive switch 2; This is the receiving unit of radar signal.Described transmit-receive switch 2 is connected with radio-frequency amplifier 6 by limiter 4, described radio-frequency amplifier 6 is connected with logarithmic detector receiver 7,6 pairs of signals of radio-frequency amplifier amplify, logarithmic detector receiver 7 is connected with the input end of AFC circuit 5 by frequency discriminator 9 simultaneously, the output terminal of described AFC circuit 5 is connected with radio-frequency amplifier 6, AFC circuit 5 is for tracking and the locking of frequency to received signal, and 9 pairs of signals of frequency discriminator are mediated; Frequently same with the reception signal with the local oscillation signal that guarantees radio-frequency amplifier 6; The output terminal of logarithmic detector receiver 7 connects the signal input part of signal acquisition process device 10, and signal acquisition process device 10 is by calculating the signal essential information.
The antenna casing is provided with the servo module 8 that control antenna 3 rotates, and described servo module 8 comprises stepper motor, scrambler and transmission shaft, and described stepper motor and scrambler are positioned at the transmission shaft both sides, and dismounting is separate, changes the unit easy operating; The output terminal of servo module 8 is connected with signal acquisition process device 10, and antenna 3 corner brace information and duty on the antenna casing are input in signal processor.
The control linkage of antenna 3 servo segments of radar: the control signal of controlling motor is provided by signal acquisition process device 10, the azimuth pitch that carries out radar rotates to be controlled, (0~360 °, orientation, 0~90 ° of pitching), orientation and pitching information code are connected to signal acquisition process device 10 by servo module 8 again simultaneously, due to the servo attitude of police radar.
Signal acquisition process device 10 is to magnetron transmitter 1 input emission trigger pip, and magnetron transmitter 1 is exported the transponder pulse signal by antenna 3 to space outerpace; Signal acquisition process device 10 extracts the amplitude of return pulse signal; Signal acquisition process device 10, according to the time of emission triggering, is adjusted the time of reception that receives signal, and by sample frequency, calculates the number of collection signal, carries out the distance of radar and calculates and intensity calculating, is output into corresponding meteorological intensity basic product.
For hardware components: signal acquisition process device 10 is controlled magnetron transmitter 1 work that triggers, transmitter magnetron output X-band frequency signal, through transmit-receive switch 2 input ends, enter into antenna 3 and then be radiated outside space, microwave signal runs into the space object reflection, reflected signal is received by antenna 3, through antenna 3, enter again the receiving end of transmit-receive switch 2, signal is sent into to radio-frequency amplifier 6 after limiter 4 decay, the signal here is by down coversion mixing intermediate frequency, pass through again the filtering of detection logarithmic receiver, detection, the echoed signal of simulation is extracted like this, by the A/D modular converter in signal acquisition process device 10, carry out digitized processing.The intermediate-freuqncy signal here is divided into two paths of signals, one tunnel is echoed signal, another road is the frequency discrimination signal, because need to carry out AFC circuit 5, control, the frequency discrimination signal, by the division of time domain, extracts microwave main broadcaster signal and echoed signal, carry out frequency ratio, comparative result is sent into to AFC circuit 5 control modules, so just, by the receive frequency of the frequency of magnetron transmitter 1 and logarithmic detector receiver 7 catching tightly, guaranteed the correctness of echoed signal.
Function for signal process part, by signal acquisition process device 10, having carried out distance processes, signal sampling frequency with 1.25MHz is as can be known, the signal distance storehouse of radar is long is 12.5m, storehouse number while processing for the full distance of radar (120Km) is as can be known is 4800, and the demonstration radius pixel of Radar Software is 300, we only need to become 300 data just passable 4800 data accumulations that gather, and through the intensity of radar apart from Logarithmic calculation:
d=log
a (x)
Wherein d is result after the intensity of radar return data is corrected; Truth of a matter when a is computing; X is real-time sampling numerical value.
Corrected the packet that later data are packaged into 310 bytes again, numerical value is given PC 11 by signal acquisition process device 10 with the udp protocol of network, PC 11 softwares will be processed later radar data again and be presented on display according to the form of matrix, and by the series of computation to base data, draw corresponding Meteorological Products (height of cloud body echo, shift to speed, intensity contour plane, quantity of precipitation, data show playback etc.), and with the pattern of Internetwork Packet Exchange, send into other computing machines of LAN (Local Area Network).
The foregoing is only preferred embodiment of the present invention, in order to limit the present invention, within the spirit and principles in the present invention not all, any modification of doing, be equal to replacement, improvement etc., within all should being included in protection scope of the present invention.
Claims (5)
1. pulse digital radar, it is characterized in that: comprise magnetron transmitter (1), signal acquisition process device (10), transmit-receive switch (2), antenna (3), limiter (4), radio-frequency amplifier (6), logarithmic detector receiver (7), AFC circuit (5), frequency discriminator (9), servo module (8);
The input end of described magnetron transmitter (1) is connected with the output terminal of signal acquisition process device (10), and the output terminal of described magnetron transmitter (1) is connected with antenna (3) by transmit-receive switch (2);
Described transmit-receive switch (2) is connected with radio-frequency amplifier (6) by limiter (4), and described radio-frequency amplifier (6) is connected with logarithmic detector receiver (7);
Described logarithmic detector receiver (7) is connected with the input end of AFC circuit (5) by frequency discriminator (9), and the output terminal of described AFC circuit (5) is connected with radio-frequency amplifier (6);
The output terminal of described logarithmic detector receiver (7) connects the input end of signal acquisition process device (10), and this signal acquisition process device (10) calculates the signal essential information;
The output terminal of described servo module (8) is connected with signal acquisition process device (10), and this servo module (8) is input to antenna (3) corner brace information and duty in signal acquisition process device (10).
2. pulse digital radar according to claim 1, it is characterized in that: described servo module (8) comprises stepper motor, scrambler and transmission shaft, and described stepper motor and scrambler are positioned at the transmission shaft both sides.
3. pulse digital radar according to claim 1, it is characterized in that: described signal acquisition process device (10) is provided with A/D modular converter and D/A modular converter.
4. pulse digital radar according to claim 1, it is characterized in that: described magnetron transmitter (1) structure comprises magnetron and connected modulation module.
5. pulse digital radar according to claim 1, is characterized in that: on described signal acquisition process device (10), be connected with PC (11).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2013102967081A CN103412311A (en) | 2013-07-15 | 2013-07-15 | Pulse digitalized radar |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2013102967081A CN103412311A (en) | 2013-07-15 | 2013-07-15 | Pulse digitalized radar |
Publications (1)
Publication Number | Publication Date |
---|---|
CN103412311A true CN103412311A (en) | 2013-11-27 |
Family
ID=49605338
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2013102967081A Pending CN103412311A (en) | 2013-07-15 | 2013-07-15 | Pulse digitalized radar |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN103412311A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105891831A (en) * | 2016-03-29 | 2016-08-24 | 成都信息工程大学 | Rapid scanning method for Doppler weather radar |
CN106997041A (en) * | 2017-05-05 | 2017-08-01 | 中国人民解放军理工大学 | Radar signal source automatic tracking system based on corner reflector |
CN107064916A (en) * | 2017-03-01 | 2017-08-18 | 中国电子科技集团公司第三十八研究所 | A kind of inexpensive variable beam mechanic scan radar |
CN107966685A (en) * | 2017-11-15 | 2018-04-27 | 北京无线电测量研究所 | The time history display methods and system that a kind of radar primary information A is shown |
CN108535700A (en) * | 2018-04-04 | 2018-09-14 | 海华电子企业(中国)有限公司 | Navigation radar transceiver device based on networking model and its working method |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4682178A (en) * | 1984-01-12 | 1987-07-21 | U.S. Philips Corporation | HF arrangement |
US4935744A (en) * | 1988-04-14 | 1990-06-19 | U.S. Philips Corporation | Coherent radar |
CN201984160U (en) * | 2011-03-11 | 2011-09-21 | 江苏北方电子有限公司 | Receiving coherent system weather radar |
CN102253373A (en) * | 2011-05-06 | 2011-11-23 | 中国电子科技集团公司第三十八研究所 | Digital phase compensation receiving system for increasing improvement factors of magnetron radars |
-
2013
- 2013-07-15 CN CN2013102967081A patent/CN103412311A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4682178A (en) * | 1984-01-12 | 1987-07-21 | U.S. Philips Corporation | HF arrangement |
US4935744A (en) * | 1988-04-14 | 1990-06-19 | U.S. Philips Corporation | Coherent radar |
CN201984160U (en) * | 2011-03-11 | 2011-09-21 | 江苏北方电子有限公司 | Receiving coherent system weather radar |
CN102253373A (en) * | 2011-05-06 | 2011-11-23 | 中国电子科技集团公司第三十八研究所 | Digital phase compensation receiving system for increasing improvement factors of magnetron radars |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105891831A (en) * | 2016-03-29 | 2016-08-24 | 成都信息工程大学 | Rapid scanning method for Doppler weather radar |
CN107064916A (en) * | 2017-03-01 | 2017-08-18 | 中国电子科技集团公司第三十八研究所 | A kind of inexpensive variable beam mechanic scan radar |
CN106997041A (en) * | 2017-05-05 | 2017-08-01 | 中国人民解放军理工大学 | Radar signal source automatic tracking system based on corner reflector |
CN107966685A (en) * | 2017-11-15 | 2018-04-27 | 北京无线电测量研究所 | The time history display methods and system that a kind of radar primary information A is shown |
CN107966685B (en) * | 2017-11-15 | 2020-07-03 | 北京无线电测量研究所 | Time history display method and system for radar one-time information A display |
CN108535700A (en) * | 2018-04-04 | 2018-09-14 | 海华电子企业(中国)有限公司 | Navigation radar transceiver device based on networking model and its working method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN102841333B (en) | CPU (Central Processing Unit) realizing method based on amplitude-comparison direction finding of multi-frequency point omnibearing passive radar | |
CN102707272B (en) | Real-time processing system for radar signals of outer radiation source based on GPU (Graphics Processing Unit) and processing method | |
US11105894B2 (en) | Weak target detection method, microwave radar sensor, and unmanned aerial vehicle | |
US10627503B2 (en) | Combined degraded visual environment vision system with wide field of regard hazardous fire detection system | |
CN104535996B (en) | Image/laser ranging/ low-altitude frequency-modulated continuous wave radar integrated system | |
CN103412311A (en) | Pulse digitalized radar | |
CN111316128A (en) | Continuous obstacle detection method, device, system and storage medium | |
CN110988862A (en) | Sensing method and system based on ultra-close distance millimeter wave radar | |
CN101031814A (en) | Frequency modulated continuous wave (FMCW) radar having improved frequency sweep linearity | |
CN201383004Y (en) | Intelligent radar for detecting traffic vehicles | |
CN104020451A (en) | Outer transmitter-based radar target track processing method based on clustering | |
CN112666543B (en) | Sparse array TDM-MIMO radar and correction method thereof | |
CN105319546A (en) | Multi-target radar and adopted digital signal processing method thereof | |
CN207008054U (en) | One-board reception/front end of emission millimetre-wave radar | |
CN106405491A (en) | Unmanned plane monitoring system based on software radio | |
CN108802734B (en) | Method and device for controlling timing synchronization of radar system | |
CN111487609A (en) | Multi-frequency continuous wave MIMO array radar system and target parameter estimation method thereof | |
RU2315332C1 (en) | Radiolocation station | |
CN104535997A (en) | Image/laser ranging/ low-altitude pulse radar integrated system | |
CN104808206A (en) | Double-line polarized pulsed Doppler weather radar system | |
CN112105951B (en) | Radar system, movable platform and control method of radar system | |
CN203299376U (en) | Radio frequency front end apparatus of portable ground surveillance radar | |
WO2023083164A1 (en) | Target tracking method and apparatus, signal fusion method and apparatus, and terminal and storage medium | |
CN107783124B (en) | Rotor unmanned aerial vehicle complex environment anti-collision radar system based on combined waveform and signal processing method | |
CN108020837B (en) | Radar, radar imaging method and device and unmanned automobile |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C12 | Rejection of a patent application after its publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20131127 |